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Emergency Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-29
Tail Cone Bleed Leak (Red TAIL CONE BLD LK CAS Message) . . . . . . . . . . . . . . . . . . . . . . 3-31
ELECTRICAL
Battery Over-Temperature (Red BATTERY O’TEMP CAS Message). . . . . . . . . . . . . . . . . 3-33.1
Dual Generator Failure (GEN OFF L-R Red CAS Message) . . . . . . . . . . . . . . . . . . . . . . . . . 3-35
FLIGHT CONTROLS
Autopilot Malfunction (Possible Red AFCS on PFD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-39
Pitch Trim Failure (Red PTRM on PFD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-39
Roll Axis Autopilot Failure (Red ROLL on PFD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-39
Pitch Axis Autopilot Failure (Red PTCH on PFD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-39
Yaw Axis Autopilot Failure (Red YAW on PFD). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-39
Aileron Trim Runaway. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-40
Rudder Trim Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-40
Pitch Trim Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-40
Hydraulic Wheel Brake Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-40
MISCELLANEOUS
Emergency Evacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-41
Ditching . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-42
Inadvertent Stall (Buffet and/or Roll-Off) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-43/3-44
510FM-07 AC 3-5.1/3-6

MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
EMERGENCY PROCEDURES
 ENGINE FAILURE OR FIRE OR MASTER WARNING OR ANY
OTHER NON-NORMAL EVENT DURING TAKEOFF
• SPEED BELOW V1 - TAKEOFF REJECTED
a. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAXIMUM PILOT EFFORT
b. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
c. Speed Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXTEND
d. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
(if runway departure is imminent)
 IF ENGINE FIRE
2. Refer to Emergency Procedures, L or R ENGINE FIRE (Engine Fire Warning Light
Illuminated).
PROCEDURE COMPLETED
 IF ENGINE FAILURE
(POSSIBLE ENGINE FAIL L-R CAS MESSAGE)
2. Refer to Abnormal Procedures, ENGINE FAILURE / PRECAUTIONARY
SHUTDOWN.
NOTE
• To obtain maximum braking performance from the antiskid system, the pilot must
apply continuous maximum effort (no modulation) to the brake pedals.
• The Takeoff Field Lengths assume that the pilot has applied maximum effort to the
brakes at the scheduled V1 speed during the aborted takeoff.
PROCEDURE COMPLETED
• SPEED ABOVE V1 - TAKEOFF CONTINUED
a. Maintain directional control.
b. ROTATE at VR to +10° initial pitch attitude (use flight director TO mode).
c. LANDING GEAR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
(after positive rate-of-climb)
d. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . V2 (single-engine) or
AS REQUIRED (multi-engine)
e. At 1500 feet AGL (minimum) and clear of obstacles. . RETRACT FLAPS at V2 +10
and ACCELERATE to VENR
(Continued Next Page)
1. Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABORT
1. Climb to a safe altitude.
510FM-07 AA 3-7
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
 ENGINE FAILURE OR FIRE OR MASTER WARNING OR ANY
OTHER NON-NORMAL EVENT DURING TAKEOFF (Continued)
 IF ENGINE FIRE INDICATIONS ARE PRESENT
(ENGINE FIRE LIGHT)
2. Refer to Emergency Procedures, L or R ENGINE FIRE (Engine Fire Warning Light
Illuminated).
PROCEDURE COMPLETED
 IF ENGINE FAILURE
(POSSIBLE ENGINE FAIL L-R CAS MESSAGE)
　
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